Hostname: page-component-cd9895bd7-fscjk Total loading time: 0 Render date: 2024-12-18T18:42:03.331Z Has data issue: false hasContentIssue false

Unsteady laminar convection in uniformly heated vertical pipes

Published online by Cambridge University Press:  29 March 2006

R. K. Gupta
Affiliation:
Prahlad Batika, Budhana Gate, Meerut-2, India

Abstract

In this paper an exact solution is presented for the problem of unsteady laminar convective flow under a pressure gradient along a vertical pipe. We have obtained the solution of the problem on the basis of the assumption that the velocity and buoyancy profiles far from the pipe entrance do not change with the height, and the entry lengths have been ignored. The wall of the pipe is heated or cooled uniformly. We have discussed both the cases, when buoyancy forces act together with the pressure gradient or in opposite direction.

In the case when the upflow is heated (or a downflow is cooled) the velocity and thermal boundary layers are formed for sufficiently large Rayleigh numbers. In the second case which has been discussed in detail (when the upflow is cooled or the downflow is heated) we have found the critical value of the Rayleigh number R = R, beyond which the velocity profile and the temperature profile become unsteady and turbulent in all the cases. In the case of the elliptical cylinder R, increases up to 1730 as the ellipticity is increased while in the case of the co-axial pipes this Rayleigh number increases as the gap c between the cylinders is decreased (if c = a/b = 1·2 then R, = 60762, but decreases to 1 when c = 4). Besides this, the time required to reach steady state increases as the Rayleigh number increases in both circular and elliptical pipes; it also increases when the eccentricity is decreased. The cases discussed by Morton (1960 and Dalip Singh (1965 are particular cases of the results derived below.

In this investigation we have dealt with the following ducts: (i) circular tubes, (ii) elliptical tubes and (iii) co-axial tubes. The general solutions for both velocity and temperature fields have been found for the case when the pressure gradient is an arbitrary function of time, with an arbitrary heat source also present. Particular cases when both the parameters are absohte constants have been discussed in detail.

We have made use of finite transforms very frequently; especially for the case of an elliptical tube, a new transform involving Mathieu functions developed by Gupta (1964 has been used. A few new infinite series have been summed with the help of this transform.

Various non-dimensional quantities (for both the cylinders) such as the Nusselt number, volume flux and rate of heat transfer have been found when the pressure gradient and source of heat generation are absolute constants.

Type
Research Article
Copyright
© 1973 Cambridge University Press

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Carslaw, H. S. & Jaegar, T. G. 1947 Conduction of Heat in Solids. Oxford University Press.
Dalip Singh 1965 Laminar convection in a heated vertical elliptical pipe. Bull. Cal. Math. Soc. 57, 109.Google Scholar
Gupta, R. K. 1964 Finite transform involving Mathieu functions and its application. Proc. Nat. Sci. Ind. 30, 779.Google Scholar
Gupta, R. K. 1972 Application of transform calculus to physical problems. D.Sc. dissertation, Agra University, India.
King, M. J. & Wiltse, J. C. 1958 Derivatives, zeros and other data pertaining to Mathieu functions. John Hopkins University, Radiation Lab. Rep. no. F 57.
Mclachlan, L. W. 1951 Theory and Applications of Mathieu Functions. Oxford University Press.
Morse, P. M. & Feshbach, H. 1953 Methods of Theoretical Physics. McGraw-Hill.
Morton, B. R. 1960 Laminar. convection in uniformly heated pipes. J. Fluid Mech. 8, 227.Google Scholar
Tao, L. N. 1961 On some laminar forced convection problems. J. Heat Tralwfer, Trans. A.S.M.E. C83, 466.Google Scholar